Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one.


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    Title :

    Linearized compressible-flow theory for sonic flight speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Heaslet, M.A. (author) / Lomax, H. (author) / Spreiter, J.R. (author)


    Publication date :

    1949


    Size :

    45 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1950


    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, Max A. / Lomax, Harvard / Spreiter, John R. | TIBKAT | 1949


    Linearized Compressible-flow Theory for Sonic Flight Speeds

    Heaslet, Max A / Lomax, Harvard / Spreiter, John R | NTRS | 1949


    Linearized Compressible Flow

    McBain, G. D. | Wiley | 2012


    Linearized potential theory of propeller induction in compressible flow

    Davidson, R.E. | Engineering Index Backfile | 1953